发明名称 Structural connection device for transmitting tensile or compressive stress between engine and mast reactor of aircraft, has connection ring connecting beams for ensuring filtering of vibrations generated by structure elements
摘要 <p>The device has a rod body whose ends are equipped with fastener covers (13, 14). The rod body comprises two beams (11, 12) that are fixed at two structure elements e.g. engine (1) and a mast reactor (5). A connection ring (17) connects the two beams in an interdependent manner for ensuring filtering of vibrations generated by the structure elements. The connection ring receives a shock absorber e.g. friction shock absorber, hydraulic damper, or pneumatic shock absorber, to partially dissipate vibrations energies in a central zone (24).</p>
申请公布号 FR2986843(A1) 申请公布日期 2013.08.16
申请号 FR20120051247 申请日期 2012.02.09
申请人 AIRBUS OPERATIONS 发明人 BROCHARD WOLFGANG;TERRAL ROMAIN
分类号 F16F7/12;B64C1/16;F16C7/04 主分类号 F16F7/12
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